In response to the requirements for modern high-speed helicopters, including high-torque capacity, significant angular misalignment compensation, and lightweight design, this paper proposes an integrated composite drive shaft design method incorporating a variable-thickness membrane disk. Firstly, Draw on existing mature ply schemes to undertake the new drive shaft design. Subsequently, by comparing the angular compensation capabilities of rectangular, circular, tapered, and trapezoidal membrane disk configurations, the optimal configuration is selected. The specific dimensional parameters of this configuration are then determined using a co-simulation optimization approach integrating ABAQUS and Isight. On this basis, guided by the principle of equal stress distribution on the membrane disk surface under extreme working conditions, a variable-thickness disk profile is designed by adopting a stepwise discrete ply-drop-off methodology from the inner to the outer region, ensuring the continuity of the primary fibers. Furthermore, finite element analysis is performed to evaluate the strength and modal characteristics of the integrated drive shaft. Experimental validation of its modal and stiffness properties is conducted, and the close agreement between the experimental results and theoretical analyses confirms the effectiveness and feasibility of the proposed design method. The findings of this study can provide a theoretical foundation for the design of drive shafts for high-speed helicopters.
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